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SAE International - AMS4050H

Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged

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Organization: SAE International
Publication Date: 3 November 2011
Status: active
description:

This specification covers an aluminum alloy in the form of plate.

Document History

AMS4050H
November 3, 2011
Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged
This specification covers an aluminum alloy in the form of plate.

References

This document references:
AMS2355 - TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
Published by SAE International on September 1, 1965
A description is not available for this item.
This document references:
AMS2772 - HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS
Published by SAE International on January 1, 1997
This specification covers requirements and recommendations for the heat treatment of wrought aluminum alloy raw materials (See 8.1.1 and 8.1.8 ). It is intended to replace MIL-H-6088.
This document references:
AS1990 - ALUMINUM ALLOY TEMPERS
Published by SAE International on January 1, 1990
A description is not available for this item.
This document references:
AS1990A - ALUMINUM ALLOY TEMPERS
Published by SAE International on May 1, 1998
The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from...
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